FIELD: aircraft rescue aids. SUBSTANCE: proposed method is based on use of parachute located in compartment in upper portion of fuselage for forming deceleration effect in aircraft landing. Method is characterized by intensification of deceleration effect due to use of two rockets of opposite direction; each rocket is located in guide barrel; use is also made of distributing mechanism for deceleration of lines. EFFECT: extended field of application; enhanced efficiency and reliability. 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR RESCUE OF AIRCRAFT | 2000 |
|
RU2211174C2 |
| AVIATION PASSENGER SELF-CONTAINED RESCUE CAPSULE | 2000 |
|
RU2171210C1 |
| HELICOPTER RESCUE FACILITY | 2000 |
|
RU2207302C2 |
| METHOD OF HELICOPTER RESCUE | 2000 |
|
RU2201383C2 |
| HELICOPTER RESCUE DEVICE | 2000 |
|
RU2201380C2 |
| METHOD OF RESCUE OF HELICOPTER | 2000 |
|
RU2203836C2 |
| AVIATION PASSENGER SELF-CONTAINED RESCUE CAPSULE | 2000 |
|
RU2171209C1 |
| METHOD OF SELF-BRAKING OF AVIATION SELF- CONTAINED PASSENGER RESCUE CAPSULE | 2000 |
|
RU2177440C2 |
| METHOD OF SELF-BRAKING OF AVIATION SELF-CONTAINED PASSENGER RESCUE CAPSULE | 2000 |
|
RU2177439C2 |
| METHOD OF HELICOPTER RESCUE | 2000 |
|
RU2201381C2 |
